N737JW

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 75,364 hrs · 44,578 cycles

SUPPLEMENTAL INFORMATION: R2 EXTERIOR EMER LIGHT INOP ; / [01] RELAMPED R2 EXTERIOR EMER LIGHT PER AMM 33-51-04. OPS GOOD.

Part: NONE — DETACHED (FWD SERVICE DOOR) · airframe 75,082 hrs · 44,407 cycles

EMERGENCY EXIT SIGN OVER FWD SER DOOR WILL NOT STAY ATTACHED ; / [01] R/R FWD SER DOOR EXIT SIGN PER AMM 33-51-01 OPS GOOD.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 73,709 hrs · 43,588 cycles

FWD ESCAPE SLIDE APPEARS LOOSE ; / R/R L1 DOOR MOUNTED ESCAPE SLIDE REF MT 725-61-06

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 73,460 hrs · 43,438 cycles

CRACK FRONT SPAR WEB SUPPORT ANGLE LOC.FWD BOOST PUMP APPROX 120 IFSS AT LT WING (1 EA). REPLACED SUPPORT ANGLE LOC FRONT SPAR WEB FWD BOOST PUMP APPROX 120 IFSS AT LT WING IAW B737700 SRM 514002 AND DRAWING #116A3001 AND 112A2004 REV A.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 73,460 hrs · 43,438 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT. REPAIRED BY WELDING SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737700 SRM 5360152R1 REPAIR 1 PARAGRAPH 4B STEP (4) AND BAC 5975

Part: ANGLE — CRACKED (LT WING TE) · airframe 73,460 hrs · 43,438 cycles

CRACK ANGLE TRAILING EDGE LOCATED WS253.0 LT WING. REPLACED ANGLE LOC WS 253.0 LT WING IAW B737700 IPC 57500025 AND SRM 514002.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 73,460 hrs · 43,438 cycles

CRACK ACCESS PANEL 651FB SUPPORT ANGLE AT RT WING. REPLACED SUPPORT ANGLE LOC AT RT WING ON ACCESS PANEL 651FB IAW B737700 SRM 514002; 511002 AND DRAWING 15A2710 REV B

Part: PLATE — CRACKED (LT WING TE) · airframe 73,460 hrs · 43,438 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED AT LEVEL WS204.25 TO WS228.25 LOWER SKIN AFT EDGE LT WING. REPLACED PLATE ASSY LOCATED AT TRAILING EDGE AREA AT LEVEL WS 204.25 AND WS 228.25 LT WING IAW B737700 SRM 514002; 511002 AND DWG 115A2001 REV B

Part: PLATE — CRACKED (LT WING TE) · airframe 73,460 hrs · 43,438 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED AT LEVEL WS253.0 TO WS278.5 LOWER SKIN AFT EDGE LT WING. REPLACED PLATE ASSY LOC AT TRAILING EDGE AREA AT LEVEL WS 253.0 AND WS 278.5 LT WING IAW B737700 SRM 514002; 511002 AND DWG 115A2001 REV.

Part: PLATE — CRACKED (LT WING) · airframe 73,460 hrs · 43,438 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 LOWER SKIN AFT EDGE LT WING. REPLACED PLATE ASSY LOC AT TRAILING EDGE AREA AT LEVEL WS 204.25 LT WING IAW SRM B737700 514002 511002 AND DWG 115A2001. REV B.

Part: RIB — CRACKED (VERICAL STAB) · airframe 73,460 hrs · 43,438 cycles

CRACK ON RIB AT LEVEL OF STA 867 ON ACCESS PANEL 321A DORSAL FIN. REPLACED RIB LOC AT LEVEL OF STA 867 ON ACCESS PANEL 321A DORSAL FIN IAW B737 700 SRM 511002 ITEM 9 AND DWG #174A1008 AND DWG #174A0101 REV

Part: ANGLE — CRACKED (LT WING TE) · airframe 73,460 hrs · 43,438 cycles

CRACK ANGLE TRAILING EDGE LOCATED WS253.0 LT WING. REPLACED ANGLE LOC ON TRAILING EDGE WS 253.0 LT WING IAW B737700 SRM 511002 PARAGRAPH 9; 514002 AND DWG 115A2930 SHEET 7 REV. ANGLE PN USED 115A29531 WITH PO # 2021 137421.

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 73,460 hrs · 43,438 cycles

CRACK STRINGER 26L BS540; WL148.5; AREA AFT FWD CARGO COMPARTMENT / REPAIRED STRINGER 26L LOC BS 500D+10' TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03 -2R-1 REPAIR 1 PARAGRAPH 4 AND DWG 143A3230 SHEET 10 REV B MADE REPAIR PARTS STRINGER SECTION (1EA) ANGLE (2EA) CHANNEL (1EA) IAW B737-700 SRM 53-00- 03-2R-1 REPAIR 1 MATERIAL USED 7075 TO/0.045' 0.050' HEAT TREATMENT REPAIR PARTS CONVERTED FROM 7075 T0 TO CONDITION T6 IAW BAC 5602 TOOL USED TEMPERATURE CONTROLLER P/N P3015GOE500000 S/N 112031023 DUE DATE 22JAN22

Part: STRINGER — CORRODED (BS 540 S27L) · airframe 73,460 hrs · 43,438 cycles

CORROSION STRINGER 27L ; BS540; WL 148.5; AREA AFT FWD CARGO COMPARTMENT / REPAIRED STRINGER 27L BS 540 WL 148.5 AREA AFT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03 -2R-1 REPAIR 1 MADE REPAIR PARTS STRINGER SECTION 2) CHANNEL 3) ANGLE (2EA) MATERIAL USED 7075 TO/ 0.056' PO # 2020-205766 AND 7075 TO/0.063' PO 2020-178589 HEAT TREATED AND CONVERTED FROM 7075 TO TO CONDITION T6 IAW BAC5602 TABLE IV PAGE 22 AND TABLE X TOOL USED TEMPERATURE CONTROLLER P/N P3015GOE500000 S/N 112031023 DUE DATE 22JAN22

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,460 hrs · 43,438 cycles

EXISTING TEMPORARY REPAIR EXTERNAL SKIN LOC AT BS 1088 AND BETWEEN STR 2L TO STR 3L AT UPPER FUSELAGE (REF N208319). REPAIRED EXTERNAL SKIN FROM BS 1084 TO BS 1092 BETWEEN STR 2L AND STR 3L I.A.W EA AE 53015621 REV 0 AND SWA EA NO.2115301134 REV IR

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 73,460 hrs · 43,438 cycles

CRACK INSPAR RIB 120.30 AT 19 INCHES FRONT SPAR LT HORIZONTAL STAB / REPAIRED INSPAR RIB 120.30 AT 19 INCHES FROM FRONT SPAR LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 73,209 hrs · 43,300 cycles

FORWARD SERVICE DOOR EMER LIGHT LENS MISSING DIRECTIONAL ARROW / REPLACED LENS ASSY REF B737 AMM 33-51-01

Part: HANDLE — BROKEN (R2 DOOR ASSIST) · airframe 72,960 hrs · 43,153 cycles

AFT SERVICE DOOR (R-2) ASSIST HANDLE BROKEN. R & R R-2 DOOR ASSIST HANDLE, PER AMM 52-13-10.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 71,834 hrs · 42,462 cycles

AFT FLASHLIGHT DOES NOT BLINK. R & R THE BATTERY IAW MM 25-64-00, OPS CHECKED OK.

Part: BATTERY PACK — FAILED (CABIN) · airframe 71,746 hrs · 42,401 cycles

RH FWD EMERGENCY LIGHTING BATTERY PACK FAILS CAPACITY TEST R&R RH FWD EMERGENCY LIGHTING BATTERY PACK PER AMM 33-51-06

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 71,736 hrs · 42,393 cycles

PASSENGER CABIN: PHOTO ALUMINATE STRIP LOOSE AT SEAT LOCATION 8C. SECURED LIGHT STRIP PER DRAWING # 33500007

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,643 hrs · 42,333 cycles

LOG PAGE ITEM 0949426 WHILE PERFORMING S.I. #12057 CRACK INDICATION FOUND USING NDT MANUAL PART 6 53-30-25 AND 53-30-18 AT S-1 AT STA. 719 INDICATION IS 4" LONG REPAIRED FUSELAGE SKIN CRACK AT STA 701 ADJACENT TO STRINGER 1 IAW AAR EA 200181 REV IR AND SWA EA 1-753-36611 REV IR.

Part: SKIN — CRACKED (FUSELAGE) · airframe 71,643 hrs · 42,333 cycles

WHILE PERFORMING SI# 12057 CRACK INDICATION FOUND USING NDT MANUAL PART 6 53-30-25 AND 53-30-018 AT S1 AT STA 719 INDICATION IS 4" LONG CRACK INDICATION FOUND TO BE AT STA 701 STRINGER 1 AND REPAIRED ON NON-ROUTINE Y190180 IAW EA 1-753-36611 REV IR

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR) · airframe 70,854 hrs · 41,817 cycles

R1 DOOR SLIDE GIRT REQUIRED ADJUSTMENT. / ADJUSTED GIRT PER MT

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 70,378 hrs · 41,514 cycles

AFT R/H FLASHLIGHT NOT BLINKING. R&R BATTERY PER AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 69,801 hrs · 41,124 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1668. / R&R BATTERY PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 69,801 hrs · 41,124 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1672. / R&R BATTERY PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,749 hrs · 41,093 cycles

LT EXTERNAL EMERGENCY LIGHT AFT OF TRAILING EDGE FLAPS INOP. R&R LAMP IAW AMM.

Part: BONDING STRAP — FRAYED (EMERGENCY EXIT) · airframe 69,749 hrs · 41,093 cycles

LT EMERGENCY EXIT DOOR BONDING STRAP FRAYED. R&R STRAP IAW SOPM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,749 hrs · 41,093 cycles

LT EMERGENCY AISLE LIGHTS INOP AT SEAT ROWS 13. R&R LIGHT IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 69,749 hrs · 41,093 cycles

EXTERNAL EMERGENCY LIGHTS INOP AT RT FORWARD AND AFT ENTRY DOORS. R&R POWER SUPPLY IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,749 hrs · 41,093 cycles

LT OVERWING EXTERNAL EMERGENCY LIGHT INOP AT EXIT DOOR. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,749 hrs · 41,093 cycles

LT EMERGENCY AISLE LIGHTS INOP AT SEAT ROWS 1. RELAMPED LIGHT IAW AMM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 69,749 hrs · 41,093 cycles

EMERGENCY AISLE LIGHT CONNECTOR D11328 AT BS. 685, STR. 3R LOOSE. R&R CONNECTOR D11328 PER SWPM & AMM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

INTERCOSTAL CORRODED AT BS. 767, S27R. R&R INTERCOSTAL PER SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

SKIN CORRODED AT BS. 907+10, STR. 22R. REPAIRED SKIN IAW ER AND EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 69,749 hrs · 41,093 cycles

VERTICAL PRESSURE WEB CRACKED AT BS. 663, RBL 40, CRACK WAS PROTRUDING FROM RIVET. REPAIRED WEB PER ER AND EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,749 hrs · 41,093 cycles

LEFT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY AT STA. 120.30, 3RD STIFFENER CRACKED. / REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 69,749 hrs · 41,093 cycles

HORIZONTAL STABILIZER R/H INSPAR RIB ASSEMBLY AT STA. 120.30, 3RD STIFFENER CRACKED. / REPAIRED STIFFENER PER SRM.

Part: ANGLE — CRACKED (BS 500A) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO COMPARTMENT BAFFLE CLIP CRACKED AT BS. 500A, LBL 21, FORWARD SIDE OF FRAME. R&R BAFFLE CLIP IAW SRM AND DWG.

Part: FITTING — CORRODED (LT HORIZ STAB) · airframe 69,749 hrs · 41,093 cycles

**CORROSION** CORROSION FOUND ON L/H HORIZONTAL STABILIZER CENTER SECTION LH FWD LOWER FORK FRONT LUG FORWARD FITTING. / REMOVED CORROSION BY REAM HOLE ON L/H HORIZONTAL STAB. CENTER SECTION L/H FWD LOWER FORK FRONT LUG. FWD FITTING IAW ENGINEERING REPAIR NO. 19-03639 REV P1 & SWA EA 1-755-4448 REV IR

Part: ATTACH FITTING — CORRODED (LT HORIZ STAB) · airframe 69,749 hrs · 41,093 cycles

**CORROSION** CORROSION FOUND ON L/H HORIZONTAL STABILIZER CENTER SECTION LH FWD LOWER FORK FRONT LUG AFT FITTING. / REMOVED CORROSION BY REAM HOLE ON L/H HORIZONTAL STAB. CENTER SECTION L/H FWD LOWER FORK FRONT LUG AFT FITTING IAW ENGINEERING REPAIR NO. 19-03639 REV P1 & SWA E.A. 1-755-4448 REV IR

Part: ATTACH FITTING — DAMAGED (VERTICAL STAB) · airframe 69,749 hrs · 41,093 cycles

VERTICAL STABILIZER R/H REAR SPAR ATTACH FITTING, ON TOP OF FUSELAGE, FORWARD OUTBOARD FAILSAFE DRAG BRACE HAD A HOLE ON INBOARD OF LUG. REPAIRED FITTING PER SRM, ER, AND EA.

Part: DRAG BRACE — CORRODED (VERTICAL STAB) · airframe 69,749 hrs · 41,093 cycles

RT VERTICAL STABILIZER REAR SPAR ATTACH FITTING AFT OUTBOARD FAIL SAFE DRAG BRACE CORRODED AT BS. 1016, RBL 2. R&R DRAG BRACE IAW DWG & SRM.

Part: ATTACH FITTING — CRACKED (VERTICAL STAB) · airframe 69,749 hrs · 41,093 cycles

LEFT VERTICAL STABILIZER REAR SPAR ATTACH FITTING, ON TOP OF FUSELAGE, FORWARD OUTBOARD FAILSAFE DRAG BRACE CRACKED ON INBOARD OF LUG. R&R DRAG BRACE IAW SRM & DWG.

Part: SKIN — WORN (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

SKIN WORN BETWEEN BS. 845 TO BS. 870, BETWEEN STR. 1R TO STR. 2R. REPAIRED SKIN PER SRM AND EA.

Part: FITTING — CORRODED (LT VERT STAB) · airframe 69,749 hrs · 41,093 cycles

***CORROSION *** ON L/H FWD VERTICAL STAB BULKHEAD FITTING FWD AND AFT FACE. BS 1016-1088; WL 250 / THE DAMAGE IS REPAIRED UNDER ATS ER 19-03669 REV IR AND EA 1-753-35239 REV IR.

Part: SKIN — OUT OF TOLERANCE (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FOUND DIAMETER OF HOLE 7L AT STR-3L TO BE OUT OF LIMITS I.A.W. CUSTOMER CARD 12107-53. HOLE DIA: O.324 IN.. LIMITS: 0.312-0.3130 IN. / REAMED HOLE 7L AT STR 3L STA 1016 TO .328 IAW CUSTOMER CARD 12107-53 STEP 20A. HOLE 7L FOUND TO BE IN TOLERANCE IAW CUSTOMER CARD 12107-53 STEP 20B.

Part: SKIN — OUT OF TOLERANCE (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FOUND DIAMETER OF HOLE 7R AT STR-3R TO BE OUT OF LIMITS I.A.W. CUSTOMER CARD 12107-53. HOLE DIA: O.326IN.. LIMITS: 0.312-0.3130 IN. / REAMED HOLE 7R AT STR 3R STA 1016 TO .328 IAW CUSTOMER CARD 12107-53 STEP 25A. HOLE 7R FOUND TO BE IN TOLERANCE IAW CUSTOMER CARD 12107-53 STEP 25B.

Part: SKIN — OUT OF TOLERANCE (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FOUND DIAMETER OF HOLE 8L AT STR-3L TO BE OUT OF LIM ITS I.A.W. CUSTOMER CARD 12107-53. HOLE DIA: O.321 I N.. LIMITS: 0.312-0.3130 IN. / REAMED HOLE 8L AT STR 3L STA 1016 TO .328 IAW CUSTOMER CARD 12107-53 STEP 20C. HOLE 8L AT STR 3L STA 1016 FOUND TO BE IN TOLERANCE IAW CUSTOMER CARD 12107-53 STEP 20D.

Part: ATTACH ANGLE — CRACKED (MLG WW) · airframe 69,749 hrs · 41,093 cycles

VAPOR BARRIER ATTACH ANGLE CRACKED. REPAIRED IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

LT LOWER FRAME WEB IS CRACKED AT BS. 727, WL 200. REPAIRED FRAME WEB PER EA.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 69,749 hrs · 41,093 cycles

BS 663 LOWER VAPOR BARRIER STIFFENER CRACKED RBL 25 / LOCATED AND DRILLED BS 663 LOWER VAPOR BARRIER STIFFENER RBL 6 TO 31 IAW SRM 51-40-05 AND DWG 111A1001 PO#746581

Part: DOUBLER — CRACKED (WHEEL WELL RH) · airframe 69,749 hrs · 41,093 cycles

SEAL RETAINER DOUBLER CRACKED AT BS 663 RBL 20 / LOCATED AND DRILLED SEAL RETAINER DOUBLER AT BS 663 RBL 20 IAW SRM 51-40-05 AND DWG 111A1000 PO # 749741

Part: FITTING — CORRODED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

***CORROSION***ON R/H FWD VERT. STAB BULKHEAD FITTING FWD AND AFT FACE / THE DAMAGE IS REPAIRED UNDER ATS ER. 19-03669 REV IR AND EA 1-753-35239 REV IR.

Part: STIFFENER — CORRODED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

***CORROSION***ON EXTERNAL STIFFENER STA1036; BETWEEN STR2L/H AND 2R/H / EXTERNAL STIFFENER AT BS 1036; BETWEEN STR 2L & 2R FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM 11'X.75'X.004. REPAIRED STIFFENER IAW ATS ER 19-03568 IR & SWA EA 1-753-35111

Part: DOUBLER — CORRODED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

***CORROSION***ON EXTERNAL SKIN DOUBLER STA1040-1072; BETWEEN STR1 AND 2R/H / EXTERNAL SKIN AT BS 1040-1072; BETWEEN STR1&2R FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1 NO ALLOWABLE LIMITS; 3.5'X2'X.005 REPAIRED DAMAGE IAW ATS ER 19-03558IR & SWA EA 1-753-35172 IR

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

***CORROSION***ON EXTERNAL SKIN STA1040-1072; BETWEEN STR2L/H AND 2R/H / EXTERNAL SKIN AT BS 1040-1072; BETWEEN STR 2L&2R FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1 (D) 3 FASTENERS IN A GROUP OF 10. 32'X15'X.005. REPAIRED DAMAGE IAW ATS ER 19-03558 IR & SWA EA 1-753-351172 IR

Part: SHEAR TIE — CORRODED (BS 219-224) · airframe 69,749 hrs · 41,093 cycles

COCKPIT WEB SHEAR TIE CORRODED BETWEEN BS. 219.8 TO BS. 224.8, LBL 40. R & R SHEAR TIE IAW SRM AND DWG.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

***CORROSION*** FUSELAGE EXTERNAL SKIN UNDER VERTICAL STABILIZER STA. 1034; STR 1-2R / FUSELAGE SKIN AT BS 1034 BETWEEN STR 1-2R FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-1 (D) 1.10'X9.75'X.004'; 3 FASTENER IN A GROUP OF 10 REPAIRED DAMAGE IAW ATS ER 19-03558 IR AND SWA EA 1-753-35172 IR

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FWD CARGO BAFFLE CRACKED BETWEEN BS. 500A TO BS. 500B, LBL21 WL. REMOVED AND REPLACED BAFFLE PER EA & SRM.

Part: NONE — CORRODED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

***CORROSION*** AT APU COMPARTMENT; STA 1121 TO 1129 BELOW S18R; WL 223 INTERNAL SIDE. ON LOWER CHORD / REPAIRED CORROSION AT THE APU COMPARTMENT; STA 1121- 1129 BELOW STR 18 R/H PER ATS ER 19-03563 REV IR + SWA EA 1-753-35105 REV IR.

Part: SUPPORT ANGLE — CORRODED (BS 359) · airframe 69,749 hrs · 41,093 cycles

MAIN ELECTRONIC AND EQUIPMENT BAY FRAME SUPPORT CLIP CORRODED AT BS. 359, BL 0. R&R SUPPORT CLIP IAW SRM AND DWG.

Part: BAFFLE — CRACKED (BS 500-500A) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO BAFFLE CRACKED BETWEEN BS. 500 TO BS. 500A, LBL 21. / R&R BAFFLE IAW SRM AND DWG.

Part: FRAME — PUNCTURED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FRAME WEB IN FLIGHT COMPARTMENT PUNCTURED AT BS. 259, S13L. REPAIRED WEB PER EA.

Part: ANGLE — CRACKED (BS 2662) · airframe 69,749 hrs · 41,093 cycles

FLIGHT COMPARTMENT CLIP CRACKED AT BS. 262, STR. 8L. R&R CLIP IAW SRM & DWG.

Part: CHANNEL — CORRODED (AFT CARGO COMPT) · airframe 69,749 hrs · 41,093 cycles

***CORROSION*** ZEE CHANNEL STA 727A-767 RBL 22 WL 156 / REMOVED AND REPLACED ZEE CHANNEL FROM STA 727A-767 RBL 22 WL 156 PER DWG# 146A7500; SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 59519U 25JUN19. CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-1. FIG. 103 DETAIL 'D.'

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,749 hrs · 41,093 cycles

AFT CARGO TRANSITION STRIP CORRODED AT FASTENER HOLE BS 887; RBL 22; WL 166 / REMOVED DAMAGE ON AFT CARGO TRANSITION STRIP (TEE ASSY) FASTENER HOLE FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE FOUND IN SRM 53-00-53-1A-2. REMOVED AND REPLACED TRANSITION STRIP (TEE ASSY) AT AFT CARGO BS 887 RBL 22 WL 156 I.A.W SRM 51-40-02-0G-0 AND DWG 146A7500 REV. B; 59600U 06-02-19

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 69,749 hrs · 41,093 cycles

***CORROSION*** AFT CARGO WASTE TANK ACCESS PANEL ATTACH ANGLE BS 867 LBL 10; WL 163 / AFT CARGO WASTE TANK ACCESS PANEL ATTACH ANGLE B.S. 867 LBL 10 WL 163 HAS CORROSION AND FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IAW SRM 51-10-02-0G-0. PART REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 AND BOEING DRAWING 149A8103 REV. D 92679U 6-30-19

Part: SHIELD — CORRODED (BS 767-790) · airframe 69,749 hrs · 41,093 cycles

AFT CARGO SHIELD FORWARD OF DOOR CORRODED BETWEEN BS. 767 TO BS. 790, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (BS 727B-767) · airframe 69,749 hrs · 41,093 cycles

ZEE CHANNEL CORRODED BETWEEN BS. 727B+10 TO BS. 767, LBL 22. R&R ZEE CHANNEL IAW SRM & DWG.

Part: CHANNEL — DAMAGED (BS 869-879) · airframe 69,749 hrs · 41,093 cycles

AFT CARGO R/H AFT Z-CHANNEL DAMAGED AT FASTENER HOLES BETWEEN BS. 869 TO BS. 879, RBL 22. / R&R ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (BS 859) · airframe 69,749 hrs · 41,093 cycles

AFT CARGO AFT SHIELD CORRODED AT BS. 859, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: STIFFENER — DEBONDED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

STIFFENER DISBONDED ON STA727B BY STRINGER S-6L / BONDED STIFFENER AT BS 727B BY STR 6L SOPM 20-50-12. 56379U 28MAY19

Part: FLOOR PANEL — DELAMINATED (E & E COMPT) · airframe 69,749 hrs · 41,093 cycles

E/E BAY FLOOR PANEL ASSY NO. 284A6223-1 IS DELAMINATED / REPAIRED E/E E BAY FLOOR PANEL P/N 284A6223-1 IAW AIPC 25-50-51-07 AND AMM 25-00-00-300-801 PARA 2I(2-8) AND BOEING RDAWING 284A6223-1

Part: STIFFENER — DEBONDED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

STIFFENER DISBONDED ON STA 727B BY STRINGER S-6R / BONDED STIFFENER AT BS 727B BY STR 6R IAW SOPM 20-50-12. 56379U 28MAY19

Part: STIFFENER — DEBONDED (AFT FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

STIFFENER DISBONDED ON STA 727C BY STRINGER S-6R / BONDED STIFFENER AT BS 727C BY STR 6R IAW SOPM 20-50-12. 56379U 28MAY19

Part: STRIP — CORRODED (AFT CARGO COMPT) · airframe 69,749 hrs · 41,093 cycles

***CORROSION*** CARGO FLOOR PANEL TRANSITION STRIP STA 727D+5 LBL 21-RBL 21 WL 156 / CORROSION ON AFT CARGO FLOOR PANEL TRANSITION STRIP STA 727D+5 LBL21-RBL21 WL 156 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS FOUND. RECEIVED NEW PART #146A9401-8. INSTALLED TRANSION STRIP IAW SRM 51-40-02 AND BOEING DRAWING 146A7500.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO FLOOR SUPPORT DAMAGED AT BS. 500C+17, RBL 2.5. R&R SUPPORT IAW SRM.

Part: WEB — CORRODED (THRESHOLD) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO DOOR LOWER THRESHOLD WEB CORRODED AT BS. 464, RBL 29. / R&R THRESHOLD WEB IAW SRM AND DWG.

Part: ANGLE — CRACKED (BS 500C) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO BAFFLE CLIP CRACKED AT BS. 500C, LBL 25. / R&R BAFFLE CLIP IAW SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 21L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW SRM AND DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,749 hrs · 41,093 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. R&R GUSSET IAW SRM AND DWG.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 69,749 hrs · 41,093 cycles

RH VAPOR BARRIER CRACKED AT BS. 663. / REPAIRED BARRIER IAW SRM.

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 69,749 hrs · 41,093 cycles

***CORROSION*** TOILET SERVICE DOOR INNER SURFACE CORRODED STA860 WL160 STR25L / REMOVED AND REPLACED TOILET SERVICE DOOR IAW AMM 52-49-07-000-801 STEPS 2C(1-2) AND IAW AMM 52-49-07-400-801 STEPS 3C1(D-F) BONDING CHECK GOOD. 56800U 04JUL19

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,713 hrs · 41,070 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED, INBOARD TOP SIDE. R&R AFT FLAP ASSEMBLY PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 69,564 hrs · 40,977 cycles

RT AFT FUSELAGE LOWER OUT SIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,323 hrs · 40,838 cycles

RT WING TRAILING EDGE-INBOARD MAIN FLAP SKIN DELAMINATED AT WBL 173 AND (1.50 INCHES) FROM TRAILING EDGE. REPAIRED FLAP SKIN PER SRM.

Part: RETAINER — LOOSE (L1 DOOR) · airframe 69,056 hrs · 40,675 cycles

L1 DOOR ESCAPE CASE GIRT BAR RETAINERS HAD LITTLE TENSION. ADJUSTED RETAINERS IAW SIP.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,315 hrs · 40,209 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,315 hrs · 40,209 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE UPPER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 68,315 hrs · 40,209 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 68,315 hrs · 40,209 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE LOWER FITTING CORRODED. REPAIRED FITTING PER EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 68,175 hrs · 40,129 cycles

LT WHEEL WELL FUSELAGE PRESSURE DECK CRACKED AT BS 663.3, LBL 32. REPAIRED DECK PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,175 hrs · 40,129 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK AT LOCATION M01669. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,175 hrs · 40,129 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK AT LOCATION M01676. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,175 hrs · 40,129 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,175 hrs · 40,129 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK AT LOCATION M01674. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,175 hrs · 40,129 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK AT LOCATION M01668. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,175 hrs · 40,129 cycles

EMERGENCY LIGHTING BATTERY PACK FAIL CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PACK PER AMM AND DWG.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 67,070 hrs · 39,427 cycles

R2 DOOR EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 66,375 hrs · 38,972 cycles

L1 DOOR GIRT BAR CLASP LOOSE. SECURED GIRT BAR PER AMM.

Part: BULKHEAD — CRACKED (BS 663) · airframe 66,105 hrs · 38,801 cycles

PRESSURE BULKHEAD CRACKED AT BS 663, RBL 46. REPAIRED THE BULKHEAD IAW EA.

Part: BRACKET — CRACKED (LOWER EXT FUSELA) · airframe 66,105 hrs · 38,801 cycles

RT WING TO BODY SUPPORT BRACKET AT WING ROOT AND WHEEL WELL CRACKED / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.

Part: BRACKET — OUT OF POSITION (R1 DOOR) · airframe 64,978 hrs · 38,097 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITON. REPOSITIONED BRACKET PER SIP.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 63,971 hrs · 37,479 cycles

FORWARD GALLEY RT SIDE EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R & R THE BATTERY IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,753 hrs · 37,339 cycles

CENTER AISLE EXIT SIGN LOOSE. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: WEB — CORRODED (BS 847-854) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY LOWER DOOR SILL WEB CORRODED BETWEEN BS 847 TO 854, STRINGER 25R. R & R THE WEB IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 500-500A) · airframe 63,087 hrs · 36,937 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO 500A, RBL 25. R & R THE SUPPORT IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,087 hrs · 36,937 cycles

SUB THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 494, RBL 28. R&R WEB ASSEMBLY IAW SRM.

Part: SUPPORT — CORRODED (BS 420-440) · airframe 63,087 hrs · 36,937 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO 440, RBL 25. R & R THE SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,087 hrs · 36,937 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 25. R&R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (BS 500A-500D) · airframe 63,087 hrs · 36,937 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO 500D, RBL 25. R & R THE SUPPORT IAW SRM.

Part: CARGO TRACK — CORRODED (BS 767-887) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY CARGO TRACK CORRODED BETWEEN BS 767+10 TO 887, RBL 12. R & R THE CARGO TRACK IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 63,087 hrs · 36,937 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 344, LBL 47. REPAIRED THE FLOOR SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 310-340) · airframe 63,087 hrs · 36,937 cycles

FORWARD ENTRY DOOR OUTBOARD THRESHOLD SUPPORT CORRODED BETWEEN BS 310 TO 340. R & R THE SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 25. R&R SUPPORT PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 63,087 hrs · 36,937 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 47. REPAIRED THE FLOOR SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 310-340) · airframe 63,087 hrs · 36,937 cycles

FORWARD ENTRY DOOR INBOARD THRESHOLD SUPPORT CORRODED BETWEEN BS 310 TO 340. R & R THE SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (BS 947) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY BULKHEAD SUPPORT ANGLE CORRODED AT BS 947.5, RBL 20. R & R THE SUPPORT ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 790, RBL 25. R&R SHIELD IAW SRM.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 847, LBL 25. R & R THE SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY SUB THRESHOLD CORRODED BETWEEN BS 794 TO BS 847, RBL 26. R&R THRESHOLD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,087 hrs · 36,937 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 TO BS 867, RBL 25. R&R SUPPORT IAW SRM.

Part: BEAM — CRACKED (BS 295) · airframe 63,087 hrs · 36,937 cycles

FORWARD SERVICE DOOR CUTOUT FORWARD LOWER STUB BEAM CRACKED AT BS. 295, WL. 209. / R&R STUB BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 63,087 hrs · 36,937 cycles

FLOORBEAM UPPER SURFACE CORRODED AT BS 986, BETWEEN RBL 25 - 47. R & R THE FLOORBEAM TEE IAW ER & SRM.

Part: CRADLE — CRACKED (FLASHLIGHT) · airframe 63,087 hrs · 36,937 cycles

FORWARD EMERGENCY FLASHLIGHT CRADLE CRACKED. R & R THE CRADLE IAW SOPM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 62,864 hrs · 36,811 cycles

R2 DOOR SLIDE PRESSURE LOW. R & R THE SLIDE IAW MT.

Part: SENSOR — FAULTY (LT WING TE FLAP) · airframe 62,448 hrs · 36,581 cycles

FLAP ASYMMETRY ON INITIAL FLAP MOVEMENT FROM 0 TO 1. DIVERTED. R & R THE NR 6 FLAP SKEW SENSOR IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT ASSY) · airframe 61,082 hrs · 35,769 cycles

FORWARD GALLEY UPPER EMERGENCY FLASHLIGHT STRAP BROKEN. REPLACED THE STRAP IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 60,967 hrs · 35,705 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MAINTENANCE.

Part: SIGN — CRACKED (CABIN) · airframe 59,113 hrs · 34,613 cycles

AFT LT GALLEY EXIT DOOR, EMER SIGN CRACKED. R & R SIGN IAW MM.

Part: LIGHT — ODOR (CABIN) · airframe 58,349 hrs · 34,198 cycles

RIGHT SIDE OVERHEAD READING LIGHT FAINT HOT ELEC SMELL AT ROW 21. FOUND PLASTIC LENS TOUCHING BULB. RELAMPED PER MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 58,267 hrs · 34,156 cycles

L1 DOOR EMER EVAC SLIDE LOOSE FROM COVER. SECURED SLIDE IAW MT.

Part: LENS — MISSING (CABIN) · airframe 58,232 hrs · 34,139 cycles

LEFT OVERWING LOWER EMER LIGHT LENS MISSING. INSTALLED LENS IAW SIP.

Part: LIGHT — DEFECTIVE (CABIN) · airframe 57,808 hrs · 33,872 cycles

AIR TURN BACK, AFTER TAKEOFF BURNING RUBBER SMELL IN AFT CABIN & COCKPIT. R & R LIGHT ASSEMBLY IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

CENTER WING SECTION WEB CRACKED AT BS 663.75, LBL 15. REPAIRED WEB IAW SRM & EA.

Part: SPAR — CRACKED (LT HORIZ STAB) · airframe 57,491 hrs · 33,675 cycles

LEFT HORIZONTAL STABILIZER FRONT SPAR WEB CRACKED BETWEEN STAB STATION 147.90 TO 157.10. REPAIRED WEB IAW SRM.

Part: PLATE — BROKEN (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

BROKEN PLATE ON FUSELAGE CUT OUT OF EXTERNAL POWER CONNECTOR DOOR. REPAIRED PLATE IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,491 hrs · 33,675 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 147.90 AT 16" FROM FRONT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,491 hrs · 33,675 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STAB STATION 129.50 AT 25.5" FROM FRONT SPAR. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 380, BETWEEN STRINGER 8L TO 7L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 727B, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 727A, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8R TO 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,491 hrs · 33,675 cycles

FRAME CRACKED AT BS 907, BETWEEN STRINGER 8L TO 9L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 55,758 hrs · 32,679 cycles

LEFT OTBD FWD INTERCOSTAL CRACKED AT BETWEEN BS 312 TO BS 328. R & R INTERCOSTAL IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,758 hrs · 32,679 cycles

M1675 EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 55,758 hrs · 32,679 cycles

R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,758 hrs · 32,679 cycles

M1674 EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 55,622 hrs · 32,605 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 55,622 hrs · 32,605 cycles

R2 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW SIP.

Part: COVER — LOOSE (CABIN) · airframe 54,696 hrs · 32,101 cycles

FORWARD EXIT LIGHT COVER LOOSE. R & R COVER IAW SIP.

Part: CIRCUIT BREAKER — POPPED (CABIN) · airframe 54,685 hrs · 32,092 cycles

AFT LT EMER LIGHT CHARGER CB POPPED. RESET CB IAW SIP.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 52,480 hrs · 30,806 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. INSTALLED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 52,342 hrs · 30,724 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: TRANSMITTER — FAULTY (COCKPIT) · airframe 51,679 hrs · 30,336 cycles

LE FLAP IN TRANSIT LIGHT & NO FLAP MOVEMENT WHEN FLAPS SELECTED TO FLAPS 5. R & R LT FLAP POSITION TRANSMITTER IAW TC.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 51,224 hrs · 30,054 cycles

RT AC BAY AFT BULKHEAD VAPOR BARRIER STIFFENER CRACKED. R & R STIFFENER PER SRM.

Part: RETAINING CLIP — LOOSE (L1 DOOR) · airframe 51,223 hrs · 30,053 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,223 hrs · 30,053 cycles

LT EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERY PACKS IAW WDM & AMM.

Part: BATTERY — FAILED (CABIN) · airframe 51,223 hrs · 30,053 cycles

RT AFT EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERIES IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 51,223 hrs · 30,053 cycles

RT EMERGENCY LIGHTS BATTERIES FAILED CAPACITY TEST. R & R BATTERY PACKS IAW WDM & AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,755 hrs · 29,790 cycles

LT WING NR 3 SLAT SKIN CRACKED AT FASTENER HOLE AT ACTUATOR ATTACH POINT. REPAIRED NR 3 SLAT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 50,755 hrs · 29,790 cycles

LT WING NR 1 SLAT SKIN CRACKED AT FASTENER HOLE AT ACTUATOR ATTACH POINT. REPAIRED SKIN PER SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 50,755 hrs · 29,790 cycles

VERTICAL PRESSURE WEB MAIN WW CRACKED AT STATION 663, BETWEEN LBL 40 TO LBL 41. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,755 hrs · 29,790 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME E-F POST 4TH FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,755 hrs · 29,790 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER APPROXIMATELY 500" BELOW CORNER RADIUS. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,755 hrs · 29,790 cycles

FLIGHT DECK RT NR 3 WINDOW FRAME E-F POST SECOND LOWER FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,755 hrs · 29,790 cycles

FLIGHT DECK LT NR 3 WINDOW FRAME E-F POST 2ND FROM BOTTOM FASTENER HOLE CRACKED. REPAIRED FRAME IAW EA.

Part: CLAMP — LOOSE (R1 DOOR) · airframe 50,116 hrs · 29,423 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR STOW CLAMPS LOOSE. SECURED CLAMPS IAW MM.

Part: LENS — MISSING (CABIN) · airframe 48,180 hrs · 28,277 cycles

AFT SERVICE DOOR EMERGENCY LIGHT LENS MISSING. INSTALLED LENS PER M/M.

Part: LIGHT — UNSECURE (CABIN) · airframe 48,138 hrs · 28,252 cycles

OVERWING AISLE EXIT LIGHT KNOCKED OFF BRACKET. RE-ATTACHED LIGHT ASSEMBLY CHECKS GOOD PER AMM 33-51-01.

Part: LENS — BROKEN (CABIN) · airframe 46,775 hrs · 27,379 cycles

R2 DOOR SIDE EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND GALLEY 4 EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN IAW MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD LAV AFT FACING WALL EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LENS IAW MM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 727E TO BS 787. REPAIRED Z-ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT LT Z-ANGLE CORRODED BETWEEN BS 727D TO BS 727E. REPAIRED Z-ANGLE IAW SRM,.

Part: ANGLE — PUNCTURED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO COMPARTMENT RT Z-ANGLE PUNCTURED AT BS 757. REMOVED AND REPLACED Z-ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED AT BS 270, BETWEEN LBL 12 TO RBL 12. REPAIRED SUPPORT IAW EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP I/B CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED CLIP IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,991 hrs · 25,776 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW EA.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 43,838 hrs · 25,690 cycles

AFT I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 43,838 hrs · 25,690 cycles

AFT I/B EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 43,598 hrs · 2,554 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GAUGE OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MT.

Part: FLOOR SKIN — PUNCTURED (FUSELAGE) · airframe 43,108 hrs · 25,277 cycles

DURING SCHEDULED OTS CHECK FOUND, FLOOR SKIN WEB PUNCTURED AT BS 236, STR 17R. REPAIRED WEB PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,399 hrs · 24,872 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,399 hrs · 24,872 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACKS FAILED. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 40,114 hrs · 23,512 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 38,833 hrs · 22,730 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: ENGINE — FAILED (NR 2) · airframe 37,581 hrs · 21,946 cycles

INFLIGHT SHUTDOWN / AIR TURNBACK / DECLARED EMERGENCY. DEPARTED BNA, NR 2 ENGINE FAILED. FOLLOWED BY A VERY LOUD BANG AND YAW OF THE AIRCRAFT. SECURED NR 2 ENGINE AND RETURNED TO BNA. REMOVED AND REPLACED NR 2 ENGINE PER MT.

Part: WEB — CRACKED (FUSELAGE) · airframe 37,074 hrs · 21,626 cycles

DURING SCHEDULED 10Y CHECK, FOUND VERTICAL WEB CRACKED AT BS 663, BETWEEN RBL 34 TO RBL 42. REPAIRED WEB PER SWA EA.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 37,074 hrs · 21,626 cycles

DURING SCHEDULED 10Y CHECK, FOUND DIAGONAL STIFFENER ANGLE CRACKED AT FWD RT MAIN WHEEL WELL BULKHEAD AT BS 663. REMOVED AND REPLACED ANGLE PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,001 hrs · 21,571 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP AT ROW 5. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,001 hrs · 21,571 cycles

DURING SCHEDULED CV CHECK, FOUND OVERHEAD EMERGENCY EXIT BULLNOSE LIGHTS INOP AT ROW 3. RELAMPED PER MM.

Part: SUPPORT FITTING — CORRODED (RT MLG) · airframe 35,874 hrs · 20,907 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 35,874 hrs · 20,907 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING CORRODED AT LWR O/B LUG FACE. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG) · airframe 35,874 hrs · 20,907 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,809 hrs · 20,863 cycles

DURING SCHEDULED HC2 CHECK, LT FWD EMERGENCY BATTERY FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,809 hrs · 20,863 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY BATTERY FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,809 hrs · 20,863 cycles

DURING SCHEDULED HC2 CHECK, RT AFT EMERGENCY BATTERY FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,809 hrs · 20,863 cycles

DURING SCHEDULED HC2 CHECK, LT AFT EMERGENCY BATTERY FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — MISSING (CABIN) · airframe 34,102 hrs · 19,834 cycles

FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT 1C. REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 34,071 hrs · 19,817 cycles

FOUND EMERGENCY EXIT BULL NOSE LIGHT LENS MISSING AT 1C. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 33,473 hrs · 19,461 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVACV SLIDE PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 3 TO LBL 5. REPAIRED FLOORBEAM CHORD PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 772, LBL 12 TO LBL 17. REPAIRED FLOORBEAM CHORD PER SWA EA.

Part: FLOOR SUPPORT — CRACKED (BS 1010-1016) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM WEB CRACKED BETWEEN BS 1010 AND BS 1016, RBL 37. REMOVED AND REPLACED FLOORBEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 927) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 927, LBL 3. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (BS 328-344 S17R) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM WEB CORRODED BETWEEN BS 328 AND BS 344, STR 17R. REPAIRED WEB PER SRM.

Part: SKIN — CORRODED (BS 505-511) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE SKIN CORRODED BETWEEN BS 505 AND BS 511, RBL 3 AND LBL 3. REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CORRODED (BS 770) · airframe 29,988 hrs · 17,409 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 770, LBL 3 AND RBL 7.5. REPAIRED FLOORBEAM PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 29,636 hrs · 17,190 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: WINDOW — LOOSE (EVAC SLIDE) · airframe 29,595 hrs · 17,164 cycles

L1 DOOR SLIDE PRESSURE IND VIEWING WINDOW LOOSE. SECURED WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,672 hrs · 16,619 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: BEARING — LOOSE (NLG ACTUATOR) · airframe 28,565 hrs · 16,551 cycles

DURING SCHEDULED HC1 CHECK, FOUND NLG ACTUATOR UPPER ATTACH POINT BEARING LOOSE. REPAIRED ACTUATOR PER SWA EA.

Part: PSEU — FAULTY (E/E BAY) · airframe 28,435 hrs · 16,482 cycles

DURING CLIMBOUT THE NLG EXTENDED WHEN GEAR HANDLE WAS PLACED IN OFF POSITION. CYCLED GEAR, OPERATED NORMAL. PSEU ILLUMINATED ON LANDING. FOUND THREE FAULTS 32-61003, 32-61010, 32-64004, RESET ALL FAULTS PER MM. R&R NOSE GEAR ACTUATOR AND NOSE GEAR LOCK ACTUATOR PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 24,417 hrs · 14,189 cycles

FOUND EEPLS STRIP LOOSE BETWEEN ROW 8 AND 10. SECURED STRIP PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 23,761 hrs · 13,789 cycles

DURING SCHEDULED HC1 CHECK, LT AND RT OVERWING EMERGENCY EXIT LIGHT BATTERY PACKS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,761 hrs · 13,789 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,761 hrs · 13,789 cycles

DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 1 DEF. RELAMPED LIGHT PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 23,761 hrs · 13,789 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST AT ROW 17 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BLADE — TORN (NR 2 ENGINE) · airframe 21,324 hrs · 12,443 cycles

DURING SCHEDULED HC2 CHECK, NR 2 ENGINE FAILED BOROSCOPE INSPECTION. SEVERAL NR 4 STAGE HPC BLADES TORN. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 20,115 hrs · 11,742 cycles

DECLARED EMERGENCY, A-HYDRAULIC SYSTEM FAILURE, QUANTITY LOSS. REMOVED AND REPLACED A-SYSTEM HYDRAULIC PUMP AND CASE DRAIN FILTERS PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 18,435 hrs · 10,799 cycles

DURING SCHEDULED 5Y CHECK, AFT LEFT AND RIGHT EMERGENCY EXIT LIGHTS FAILED OP CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 18,299 hrs · 10,719 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVERS AT ROW 2 ABC, ROW 8 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 17,848 hrs · 10,501 cycles

EEPLS COVER AT ROW 1 ABC, MISSING. INSTALLED EEPLS COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,030 hrs · 10,069 cycles

DURING SCHEDULED RON CHECK, FOUND EMERGENCY EXIT LIGHTS AT L1 DOOR AND R1 DOOR, EEPLS AT ROW 2ABC TO 5ABC INOP. REMOVED AND REPLACED FWD RT BATTERY PACK PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,724 hrs · 9,907 cycles

EEPLS COVER BROKEN AT FWD SECTION. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 13,035 hrs · 7,760 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,035 hrs · 7,760 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED THROUGHOUT CABIN. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 8,500 hrs · 5,137 cycles

EEPLS COVER LOOSE AT FWD CABIN. SECURED COVER PER MM.

Part: BRACKET — OUT OF ADJ (CABIN) · airframe 5,878 hrs · 3,551 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. RE-ADJUSTED GIRT BRACKET PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY) · airframe 5,067 hrs · 3,084 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. REPOSITIONED EVAC SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,960 hrs · 1,826 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AND MISSING LENS AT FWD END. RELAMPED AND INSTALLED LENS PER MM.

Part: DOOR — UNSECURED (PAX DOOR)

AIR TURNBACK, PRESSURIZATION LEAK AT FWD ENTRY DOOR. UNABLE TO CONTROL MANUALLY THE ACFT PRESSURIZATION. DOOR APPEARED NOT BEING COMPLETELY CLOSED, DOOR ANNUNCIATOR DID NOT ILLUMINATE. C/W GROUND PRESS LEAK CK. OPS CK GOOD, DOOR OPS CK GOOD.